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公开(公告)号：EP4458672A1
公开(公告)日：2024-11-06
申请号：EP24171229.8
申请日：2024-04-19
IPC分类号： B64D11/00 , B64D11/06 , H04N21/414
摘要： An in-flight entertainment, IFE, system (200) may include a structural panel (204) supporting one or more aircraft seat components. The one or more aircraft seat components may include a primary IFE display and a secondary IFE display. Both the primary IFE display and the secondary IFE display may be coupled to a portion of the structural panel (204) facing the passenger. The primary display (206) may receive and display a plurality of in-flight related content from at least one IFE source, while the secondary display (208) may receive and display a plurality of media content associated with a personal electronic device, PED (202), of the passenger. The IFE system may also include at least one controller which is in communication with at least one of the primary IFE display, the secondary IFE display, and the PED. The controller may selectively display content received from at least one of the IFE source or the PED (202).
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公开(公告)号：EP4443749A1
公开(公告)日：2024-10-09
申请号：EP24166015.8
申请日：2024-03-25
CPC分类号： H04B1/0003 , H04B7/22 , H04W40/12
摘要： Techniques for selecting frequencies of operation are described. HF signals may land at the receiver node with power levels dependent upon the transmit frequency. The frequency with the highest power level at the receiver node may be selected when the receiver node is not subject to interfering. The receiver node may be unable to receive a desired signal if an interfering signal has a signal level which is higher than the desired signal. The transmitter node may select a frequency which has a receiver signal level which is higher than the interfering signal for the selected frequency. The receiver node may then receive the transmit signal at the selected frequency even when subject to interfering from the interferer node.
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公开(公告)号：EP4439124A1
公开(公告)日：2024-10-02
申请号：EP24166715.3
申请日：2024-03-27
IPC分类号： G01S13/933 , G01S7/41 , G01S13/91 , G08G5/00
CPC分类号： G01S7/412 , G01S13/933 , G01S2013/91620130101 , G08G5/0082 , G08G5/0013 , G08G5/0026
摘要： A system (100) for detecting threats at an area is disclosed. The system (100) may include a controller (102) including one or more processors (106) configured to execute a set of program instructions stored in a memory (104). The set of program instructions may be configured to cause the one or more processors to receive safe historical data of an area configured to be representative of a lack of threats, receive new data of the area from one or more nodes, compare the new data and the safe historical data to identify a difference between the new data and the safe historical data, and update a database based on the difference.
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公开(公告)号：EP4434893A1
公开(公告)日：2024-09-25
申请号：EP24164882.3
申请日：2024-03-20
IPC分类号： B64D25/10
CPC分类号： B64D25/10
摘要： A method is disclosed herein. The method includes receiving, by a processor, a first acceleration data from an accelerometer (244), calculating, by the processor, a change in velocity based on the first acceleration data, the change in velocity being calculated over a first period of time, and adjusting, by the processor, a timing sequence based on the change in velocity.
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5.发明公开
公开(公告)号：EP4418018A1
公开(公告)日：2024-08-21
申请号：EP24157573.7
申请日：2024-02-14
CPC分类号： G01S19/215 , G01S19/15 , G01S19/49
摘要： A system and method for detection of GNSS signal spoofing with high integrity error bounding determines a parity space formulation for coordinates of a GNSS-driven master position solution (e.g., fully absolute/GNSS or blended GNSS/IRS solution) and a corresponding coasted position solution (e.g., less frequently GNSS-updated), wherein a parity vector expresses consistency of the master coordinate with the coasted coordinate. Based on a desired level of missed detection, protection levels are determined for the parity space formulation, and integrity bounds on the master and coasted solutions calculated. The parity vector is compared with a detection threshold. If, for any solution component (e.g., direction, axis) of the master solution, the parity vector meets or exceeds the threshold, a spoofer is detected and a coasted solution is propagated with its coasted integrity bound. If no spoofer is detected, the master solution and its master integrity bound are propagated as output.
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公开(公告)号：EP4393768A1
公开(公告)日：2024-07-03
申请号：EP23209527.3
申请日：2023-11-13
CPC分类号： B60L58/16 , B60L58/12 , B60L2200/1020130101 , B60L2240/54720130101 , B60L2240/54520130101 , B60L2260/5220130101 , B60L2260/5420130101
摘要： A system and for performance prediction of an electric aircraft is disclosed. The system may include a controller (102) including one or more processors configured to execute a set of program instructions stored in a memory. The set of program instructions may be configured to cause the one or more processors to receive aircraft data, route data, and environmental data. The aircraft data may include battery data of the battery of the electric aircraft. The system may also be configured to predict an available range based on the aircraft data and the environmental data.
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公开(公告)号：EP4369165A1
公开(公告)日：2024-05-15
申请号：EP23209238.7
申请日：2023-11-10
IPC分类号： G06F3/04855 , G06F3/04883 , G06F3/04886
CPC分类号： G06F3/04855 , G06F3/04883 , G06F3/04886
摘要： A system and method for controlling a scrolling function in a touchscreen display (104) defines a touch sensitive region for the scrollbar. When the touch sensitive region receives a press-and-hold input, the system renders large directional inputs for the corresponding window / list selection window and enters a persistent state wherein the directional inputs supersede the scrolling function. The scrollbar input may be deactivated during the persistent state. The persistent state is exited when the user makes a selection outside the directional inputs. The system may define press-and-hold touch sensitive regions larger than the touch sensitive region for the scrollbar generally. The larger press-and-hold regions may be associated with, and extend beyond, a currently active window / dialog box.
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公开(公告)号：EP4342802A1
公开(公告)日：2024-03-27
申请号：EP23198598.7
申请日：2023-09-20
发明人： LAHR, Weston J. , RADEMAKER, Richard M. , PERKINS, Aaron , WILSON, Brandon E. , LJUNGKRANTZ-LAHR, Charlotte S.
IPC分类号： B64D45/00 , B64D45/04 , B64D45/08 , G06V20/50 , G06V20/56 , G06V20/60 , G06V20/64 , G06V20/70 , G08G5/00 , G08G5/02 , G01C23/00
摘要： A system includes at least one camera (114) implemented in an aircraft, the at least one camera (114) configured to capture images external to the aircraft. The system further includes at least one processor (116) implemented in the aircraft, one or more of the at least one processor (116) communicatively coupled to the at least one camera (114), the at least one processor (116) configured to: receive the images from the at least one camera (114); identify visual references in at least one of the images; and output an annunciation instruction configured to cause an annunciation to a pilot that the visual references have been identified by the at least one processor (116).
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公开(公告)号：EP4328871A1
公开(公告)日：2024-02-28
申请号：EP23193178.3
申请日：2023-08-24
摘要： A method for non-invasive operator health monitoring is disclosed. The method may include receiving at least one of one or more images or one or more videos (104) of tracked one or more facial features of a pilot from one or more pilot monitoring devices. The one or more tracked facial features may include at least one of a pilot's eyes, mouth, head posture, forehead, or cheek. The method may include determining at least one of one or more eye tracking parameters, one or more mouth tracking parameters, one or more head tracking parameters, or an emotion of the pilot. The method may include determining a pilot health monitoring value based on at least one of the determined one or more eye tracking parameters, the determined one or more mouth tracking parameters, the one or more head tracking parameters, or the determined emotion of the pilot.
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10.发明公开
公开(公告)号：EP4306411A1
公开(公告)日：2024-01-17
申请号：EP23185612.1
申请日：2023-07-14
发明人： ROTHWELL, Trevis J.
IPC分类号： B64D11/00
摘要： A system includes an aircraft interface device, displays installed in an aircraft cabin, an LRU, and a mobile device within the aircraft cabin. The mobile device is configured to: capture images of the aircraft cabin; identify at least one display of the at least two displays within the captured images; display an augmented reality view of the captured images including indicator(s) for the at least one display having user-selectable video content options; receive a user selection of a given display of the at least one display (104), indicative of a selection to control video content for the given display; display a graphical representation of the user-selectable video content options; receive a user option selection of the user-selectable video content options, the user option selection associated with a particular video content option associated with particular video content; and transmit an instruction to display the particular video content on the given display.
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