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公开(公告)号：US11137774B2
公开(公告)日：2021-10-05
申请号：US16453470
申请日：2019-06-26
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dorothee De Villele , Michal Polansky , Marek Batelka , Laurent Villacampa
Abstract: Systems and methods are provided for managing speed-constrained vehicle operations. One exemplary method of operating an aircraft involves identifying a speed constraint associated with a navigational reference point, determining a speed envelope region en route to the navigational reference point based at least in part on the first speed constraint, identifying a target speed en route to the navigational reference point, and determining a speed profile for autonomously operations en route to the navigational reference point within the speed envelope region. The speed profile intersects the target speed within the speed envelope region and a slope of the speed profile is influenced by the target speed, for example, to effectuate or approximate the target speed by increasing the duration of time operation at or around the target speed is achieved. In one or more embodiments, multiple different target speeds associated with different flight levels or operating regions are accounted for.
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公开(公告)号：US10388170B2
公开(公告)日：2019-08-20
申请号：US15676003
申请日：2017-08-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dorothee De Villele , Michal Polansky , Marek Batelka , Laurent Villacampa
Abstract: Systems and methods are provided for managing speed-constrained vehicle operations. One exemplary method of operating an aircraft involves identifying a speed constraint associated with a navigational reference point, determining a speed envelope region en route to the navigational reference point based at least in part on the first speed constraint, identifying a target speed en route to the navigational reference point, and determining a speed profile for autonomously operations en route to the navigational reference point within the speed envelope region. The speed profile intersects the target speed within the speed envelope region and a slope of the speed profile is influenced by the target speed, for example, to effectuate or approximate the target speed by increasing the duration of time operation at or around the target speed is achieved. In one or more embodiments, multiple different target speeds associated with different flight levels or operating regions are accounted for.
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公开(公告)号：US20200058226A1
公开(公告)日：2020-02-20
申请号：US16453470
申请日：2019-06-26
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dorothee De Villele , Michal Polansky , Marek Batelka , Laurent Villacampa
Abstract: Systems and methods are provided for managing speed-constrained vehicle operations. One exemplary method of operating an aircraft involves identifying a speed constraint associated with a navigational reference point, determining a speed envelope region en route to the navigational reference point based at least in part on the first speed constraint, identifying a target speed en route to the navigational reference point, and determining a speed profile for autonomously operations en route to the navigational reference point within the speed envelope region. The speed profile intersects the target speed within the speed envelope region and a slope of the speed profile is influenced by the target speed, for example, to effectuate or approximate the target speed by increasing the duration of time operation at or around the target speed is achieved. In one or more embodiments, multiple different target speeds associated with different flight levels or operating regions are accounted for.
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公开(公告)号：US20190051189A1
公开(公告)日：2019-02-14
申请号：US15676003
申请日：2017-08-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dorothee De Villele , Michal Polansky , Marek Batelka , Laurent Villacampa
CPC classification number: G08G5/0052 , G01C21/00 , G01C21/14 , G01C21/20 , G01C21/3492 , G01C23/00 , G05D1/101 , G08G5/0021 , G08G5/0034
Abstract: Systems and methods are provided for managing speed-constrained vehicle operations. One exemplary method of operating an aircraft involves identifying a speed constraint associated with a navigational reference point, determining a speed envelope region en route to the navigational reference point based at least in part on the first speed constraint, identifying a target speed en route to the navigational reference point, and determining a speed profile for autonomously operations en route to the navigational reference point within the speed envelope region. The speed profile intersects the target speed within the speed envelope region and a slope of the speed profile is influenced by the target speed, for example, to effectuate or approximate the target speed by increasing the duration of time operation at or around the target speed is achieved. In one or more embodiments, multiple different target speeds associated with different flight levels or operating regions are accounted for.
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