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公开(公告)号：US11767126B2
公开(公告)日：2023-09-26
申请号：US16836330
申请日：2020-03-31
IPC分类号： G06F3/0482 , B64D43/00 , G06F16/901 , G06F9/48 , G06F3/04817
CPC分类号： B64D43/00 , G06F3/0482 , G06F3/04817 , G06F9/4881 , G06F16/9024
摘要： Disclosed are methods, systems, and non-transitory computer-readable medium for automatic time keeping of an electronic checklist. One method may include: receiving a user and/or system input associated with a graphical user interface (GUI) of an electronic checklist; determining whether the user and/or system input triggers a timer event; in response to determining that the user and/or system input triggers the timer event, determining whether the timer event is a first type of timer event or a second type of timer event; in response to determining that the timer event is the first type of timer event, performing a first timer process; and in response to determining that the timer event is the second type of timer event, performing a second timer process.
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公开(公告)号：US11734630B2
公开(公告)日：2023-08-22
申请号：US17658845
申请日：2022-04-12
IPC分类号： G06F3/0482 , G06Q10/0631 , G06F16/26 , G06Q50/30 , G06F9/451 , G06F16/22 , G06F3/0484
CPC分类号： G06Q10/06316 , G06F3/0482 , G06F3/0484 , G06F9/453 , G06F16/2291 , G06F16/26 , G06Q50/30
摘要： Disclosed are methods, systems, and non-transitory computer-readable medium for electronic checklist data references. For instance, the method may include: displaying, in a GUI, a checklist GUI corresponding to a checklist of an electronic checklist system; determining whether the checklist includes one or more dynamic data references and/or one or more static data references; in response to determining the checklist includes the one or more dynamic data references, performing a dynamic data reference process to display specific data in the checklist GUI for the one more dynamic data references; and in response to determining the checklist includes the one or more static data references, displaying one or more static data fields in the checklist GUI for the one or more static data references to initiate performing a static data reference process for the one or more static data fields.
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公开(公告)号：US11334829B2
公开(公告)日：2022-05-17
申请号：US16720430
申请日：2019-12-19
IPC分类号： G06F3/0482 , G06Q10/06 , G06F16/26 , G06Q50/30
摘要： Disclosed are methods, systems, and non-transitory computer-readable medium for electronic checklist data references. For instance, the method may include: displaying, in a GUI, a checklist GUI corresponding to a checklist of an electronic checklist system; determining whether the checklist includes one or more dynamic data references and/or one or more static data references; in response to determining the checklist includes the one or more dynamic data references, performing a dynamic data reference process to display specific data in the checklist GUI for the one more dynamic data references; and in response to determining the checklist includes the one or more static data references, displaying one or more static data fields in the checklist GUI for the one or more static data references to initiate performing a static data reference process for the one or more static data fields.
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4.发明申请公开(公告)号：US20180233056A1
公开(公告)日：2018-08-16
申请号：US15433272
申请日：2017-02-15
CPC分类号： G08G5/025 , B64D45/04 , G01C23/00 , G08G5/0021 , G09G5/363 , G09G5/38 , G09G2340/0464 , G09G2380/12
摘要： Cockpit display systems and methods are provided for generating energy management symbology on cockpit displays, which aid pilot decision-making when evaluating and executing direct approaches. In an embodiment, the cockpit display system includes a cockpit display device on which a first cockpit display, such as a vertical situation display or a horizontal navigation display, is generated. A controller is operably coupled to the cockpit display device and configured to: (i) identify a direct approach (DA) path to a configuration point located over a destination airfield; (ii) calculate a first DA energy estimate for the aircraft to fly the DA path under engine idle conditions and arrive at the configuration point with an airspeed less than a configuration airspeed; and (iii) generate symbology on the first cockpit display indicative of the first DA energy estimate.
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公开(公告)号：US12033250B2
公开(公告)日：2024-07-09
申请号：US18048726
申请日：2022-10-21
发明人： Barbara Holder , Michael Dillard , Stephen Whitlow
IPC分类号： G06T11/20 , B64D43/00 , G06F3/04842
CPC分类号： G06T11/206 , B64D43/00 , G06F3/04842
摘要： Methods and systems are provided for displaying visualizations of a vehicle's capability with respect to an input query corresponding to a prospective action to modify operation of the vehicle. One method involves identifying one or more input query parameters, obtaining current status information for the vehicle, identifying one or more performance constraints for the vehicle, and determining a capability envelope for the vehicle for satisfying the one or more input query parameters for the prospective action based at least in part on the current status information and the one or more performance constraints. The capability envelope includes a plurality of potential trajectories for the vehicle different from a reference trajectory for the vehicle. The method provides graphical indicia of the one or more input query parameters and the capability envelope with respect to the reference trajectory on a navigational map display.
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公开(公告)号：US11538203B2
公开(公告)日：2022-12-27
申请号：US17316384
申请日：2021-05-10
发明人： Barbara Holder , Michael Dillard , Stephen Whitlow
IPC分类号： G06T11/20 , B64D43/00 , G06F3/04842
摘要： Methods and systems are provided for displaying visualizations of a vehicle's capability with respect to an input query corresponding to a prospective action to modify operation of the vehicle. One method involves identifying one or more input query parameters, obtaining current status information for the vehicle, identifying one or more performance constraints for the vehicle, and determining a capability envelope for the vehicle for satisfying the one or more input query parameters for the prospective action based at least in part on the current status information and the one or more performance constraints. The capability envelope includes a plurality of potential trajectories for the vehicle different from a reference trajectory for the vehicle. The method provides graphical indicia of the one or more input query parameters and the capability envelope with respect to the reference trajectory on a navigational map display.
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7.发明授权公开(公告)号：US11532235B2
公开(公告)日：2022-12-20
申请号：US16598026
申请日：2019-10-10
IPC分类号： G08G5/00 , B64D45/00 , G01C21/20 , G06F3/0482 , G06F3/04815
摘要： A flight deck system for providing task management assistance in managing the flight path to the flight crew is provided. The system is configured to: mine flight plan data for a current flight plan, navigational data, and vertical situation display (VSD) data; obtain notification data items originating from onboard avionics systems and systems external to the aircraft that indicate upcoming conditions that will affect the current flight plan; automatically analyze the mined flight plan data and the notification data items to identify a sensed deviation condition; automatically identify an aircraft-related deviation condition from an aircraft failure event; receive flight crew notification of a non-sensed deviation condition; automatically generate a plurality of flight plan deviation options to accommodate a sensed deviation condition, an aircraft-related deviation condition, or a non-sensed deviation condition; and present graphical elements representative of the flight plan deviation options to the flight crew on an integrated interactive graphical user interface.
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公开(公告)号：US11472567B2
公开(公告)日：2022-10-18
申请号：US17002904
申请日：2020-08-26
摘要： Methods and systems for automating processes of receiving, prioritizing, and grouping weather data into a weather event, extent of weather event, and an associated duration for presentation on a displayed mission timeline in an aircraft having a flight plan (FP). The method includes: receiving, by a controller circuit, weather data, aircraft state data, and aircraft system status data; identifying a weather phenomenon that impacts the FP and creating an information structure for the weather phenomenon, the information structure including at least a type, a subtype, a severity, a start of impact and an end of impact. The method also includes presenting a weather event indicator overlaid on the mission timeline to indicate the weather phenomenon. The rendering of the weather event indicator on the mission timeline additionally depicts on the mission timeline: a start, an end, and duration of the weather event.
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公开(公告)号：US10388171B2
公开(公告)日：2019-08-20
申请号：US15433272
申请日：2017-02-15
摘要： Cockpit display systems and methods are provided for generating energy management symbology on cockpit displays, which aid pilot decision-making when evaluating and executing direct approaches. In an embodiment, the cockpit display system includes a cockpit display device on which a first cockpit display, such as a vertical situation display or a horizontal navigation display, is generated. A controller is operably coupled to the cockpit display device and configured to: (i) identify a direct approach (DA) path to a configuration point located over a destination airfield; (ii) calculate a first DA energy estimate for the aircraft to fly the DA path under engine idle conditions and arrive at the configuration point with an airspeed less than a configuration airspeed; and (iii) generate symbology on the first cockpit display indicative of the first DA energy estimate.
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公开(公告)号：US20220017232A1
公开(公告)日：2022-01-20
申请号：US17002904
申请日：2020-08-26
发明人： Jan Bilek , Petr Talla , Barbara Holder , Girish Benakatti , Martina Tucková
摘要： Methods and systems for automating processes of receiving, prioritizing, and grouping weather data into a weather event, extent of weather event, and an associated duration for presentation on a displayed mission timeline in an aircraft having a flight plan (FP). The method includes: receiving, by a controller circuit, weather data, aircraft state data, and aircraft system status data; identifying a weather phenomenon that impacts the FP and creating an information structure for the weather phenomenon, the information structure including at least a type, a subtype, a severity, a start of impact and an end of impact. The method also includes presenting a weather event indicator overlaid on the mission timeline to indicate the weather phenomenon. The rendering of the weather event indicator on the mission timeline additionally depicts on the mission timeline: a start, an end, and duration of the weather event.
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