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公开(公告)号:US10225349B2
公开(公告)日:2019-03-05
申请号:US15334822
申请日:2016-10-26
Applicant: Honeywell International Inc.
Inventor: Matej Dusik , John Beckwith , John Hajdukiewicz , Filip Magula , Frantisek Mikulu , Jiri Vasek
Abstract: A server system for an aircraft is provided. In one embodiment, the server system comprises an aircraft server unit that is operative to receive data from one or more data sources, and a software development kit (SDK) application server in operative communication with the aircraft server unit. The SDK application server comprises one or more processing core modules configured to process the data from the one or more data sources, and one or more application modules including one or more aircraft tablet device logic modules that are configured to respectively execute one or more aircraft tablet device applications. The data processed by the one or more processing core modules is separated from the one or more aircraft tablet device logic modules. The SDK application server is configured to communicate with one or more external portable computing devices.
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公开(公告)号:US09884690B2
公开(公告)日:2018-02-06
申请号:US15145346
申请日:2016-05-03
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zdenek Moravek , Katerina Sprinarova , David Kunes , Filip Magula
CPC classification number: B64D45/00 , G08G5/0013 , G08G5/0021 , G08G5/0091 , G08G5/025 , G08G5/065
Abstract: Methods and systems are provided for facilitating analysis and selection of a destination for operating a vehicle. One exemplary method facilitating analysis of landing an aircraft at an airport involves displaying a map of the airport that includes a graphical representation of a runway at the airport, determining a runway viability parameter for the runway using current status information associated with one or more of the aircraft and the airport, and displaying indicia of the runway viability parameter on the map in graphical association with the graphical representation of the runway, thereby providing indication of the value or state of the runway viability parameter for that runway on the airport map.
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公开(公告)号:US20170243495A1
公开(公告)日:2017-08-24
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
CPC classification number: G08G5/0021 , B64C9/38 , G05D1/0676 , G08G5/0013 , G08G5/0039 , G08G5/0091 , G08G5/025
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.
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公开(公告)号:US20170229024A1
公开(公告)日:2017-08-10
申请号:US15019650
申请日:2016-02-09
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zdenek Moravek , David Kunes , Filip Magula , Robert Sosovicka , Katerina Sprinarova
IPC: G08G5/00
CPC classification number: G08G5/0039 , G01C21/20 , G01C23/00 , G08G5/0013 , G08G5/0021 , G08G5/0047 , G08G5/0091 , G08G5/025
Abstract: Methods and systems are provided for generating a route that facilitates navigating a vehicle to a diversion destination while satisfying applicable safety thresholds or other constraints, such as a maximum landing weight. One exemplary method of facilitating an aircraft landing at a diversion airport involves obtaining a current position of the aircraft, identifying a landing threshold influenced by a characteristic of the aircraft, obtaining one or more constraints associating with diverting to the diversion airport, and determining a route from the current position to the diversion airport based at least in part on the landing threshold and the one or more constraints. The route satisfies the constraints and results in a predicted value for the aircraft, e.g., a predicted aircraft landing weight, that satisfies the landing threshold. A graphical representation of the route is displayed on a display device onboard the aircraft.
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