Abstract: The present disclosure relates to a system that comprises: a control station intended to be operated; an unmanned aerial vehicle for multiple tasks (UAM) which is supported, by unmanned aerial devices (UAV), unmanned ground vehicle (UGV), and by a centralised mobile reel unit which feeds cables and hoses for supplying multiple additive and subtractive fluids (e.g. paint, air suction, etc.) and for charging power; wherein the cables and hoses comprise a device that makes it possible to predict trajectories, without interfering with flight maneuvers or the environment. The UAM comprises a robotic arm with specific tools that make it possible, for example, to paint fences, as well as a device that allows it to be attached to various surfaces.

Abstract: Methods, systems, and devices for wireless communications are described. A wireless device may receive a broadcast remote identification (BRID) message from a unmanned aerial vehicle (UAV), where the BRID message may include an identity of the UAV. The wireless device may identify UAV information associated with the UAV based on the UAV ID. In some cases, the wireless device may be configured with information that enables the identification of the UAV information. In other cases, the wireless device may request the UAV information from a network entity, such as a UAV flight management system (UFMS), which provides the requested UAV information. In some examples, the UFMS may request the UAV information from an unmanned aerial system (UAS) service supplier (USS) based on the BRID information. Upon identifying the UAV information, the wireless device may broadcast the UAV information to manned aerial vehicles, thereby indicating a presence of the UAV.

Abstract: The invention relates to an electronic display device on board an aircraft capable of landing or maintaining a hover above a landing zone and comprising: a module for calculating a distance between the aircraft and the landing zone according to a horizontal direction and for determining a height of the aircraft; and a module for displaying an exocentric aircraft symbol, positioned at a distance said exocentric from the aircraft according to an exocentric direction and at a height difference said exocentric relative to the aircraft, the display module being further configured to display an exocentric landing zone symbol, positioned at a distance from the landing zone equal to the exocentric distance according to the exocentric direction and at the same height as the exocentric aircraft symbol.

Abstract: The present disclosure describes displaying on a flight deck (12) graphical presentations indicative of performance limitations of an aircraft (10) resulting from an in-flight aircraft reconfiguration. The graphical presentations are co-located on the flight deck (12) with the graphical presentations of the aircraft (10) and/or system (34) parameters to which the performance limitations apply.

Abstract: A system and methods for enhancing operator situational awareness are disclosed. For example, one method includes monitoring a plurality of radio transmissions associated with a plurality of vehicles in a first traffic flow pattern, monitoring a second traffic flow pattern in a vicinity of a vehicle of the plurality of vehicles, monitoring at least one weather value for a destination site for the plurality of vehicles, proposing a destination approach for the vehicle in response to the monitoring, evaluating an impact of the proposed destination approach on an existing travel path for the vehicle, and generating a second travel path for the vehicle in response to the evaluating.

Abstract: Methods, systems, and apparatus, including computer programs encoded on a computer storage medium, for receiving aircraft transponder signals. Identifying, from among the aircraft transponder signals, a first aircraft transponders signal based on an identifier, wherein the identifier indicates that the first aircraft transponder signal is associated with an aircraft on which the computing system is located. Identifying first location data within the first aircraft transponder signal. Generating second location data by converting the first location data to a format recognizable by a geographic mapping application, where the second location data is readable by the geographic mapping application to permit the geographic mapping application to present a graphical representation of a geographical location of the aircraft as represented by the first location data. Providing the second location data to the geographic mapping application for presentation to a user.

Abstract: A system for displaying information relative to an aircraft flight and related method are provided. This system comprises a display device, and a module for managing the display on the display device, the management module being configured for controlling the display, on a window of the display device, of a timescale representative of a time period of the flight, and for controlling the display, facing the timescale, of pieces of information relative to a series of events intended to occur in a time window comprised in the time period. The module for managing the display is configured for determining a position in time of the time window comprised in the time period and a duration of the time window, and for controlling the display, along the timescale, of a marker representative of the position in time and of the duration of the time window.

Abstract: A vehicle control system includes at least one control inceptor to provide pilot control of an associated vehicle and a communications interface to process external entity SA data associated with an external entity that is received at a communications system associated with the associated vehicle. An SA video screen displays video data to a pilot of the associated vehicle. The video data includes pilot-perspective visual data corresponding to a real-time dynamic virtual representation of surroundings of the associated vehicle that simulates a real-world visual perspective of the pilot to the surroundings of the associated vehicle and is responsive to the pilot control. A visual indicator of the external entity is superimposed onto the pilot-perspective visual data at an approximate location corresponding to an actual location of the external entity relative to the associated vehicle and beyond a visual range of the pilot based on the external entity SA data.

Abstract: A system for monitoring the integrity of a plurality of ground conductors has a plurality of monitors, with a different monitor associated with each ground conductor. Each monitor includes a voltage sensor which monitors voltage on a closed circuit of the monitor. Upon the voltage sensor sensing an unexpected voltage, a transmitter of the monitor issues an “alarm” signal, which may be wireless (e.g., being sent using LoRaWAN protocol). The transmitter may issue other signals, including a periodic “heartbeat” signal to confirm continued operation of the monitor, and a “movement” signal to indicate movement of the monitor. The monitor may be GPS-enabled, in which case each signal may include the GPS coordinates of the monitor. The signals issued by the transmitter may ultimately be analyzed by an operator via a user interface platform, which may simultaneously display information regarding two or more of the plurality of monitors.

Abstract: Controlling and reconfiguring a display system that includes at least two screens that are installed in a cockpit of an aircraft in case of a failure of one of the screens. For example, a control unit of the display system may detect occurrence of a screen failure. In response to detecting the screen failure, the control unit may determine whether a critical flight relevant information has not been displayed on an operational screen during a predetermined period of time, and in response to determining that the critical flight relevant information has not been displayed on the operational screen during the predetermined period of time, command display of a message on the operational screen that suggests displaying the critical flight relevant information on the operational screen.

Abstract: Devices, systems, and methods for determining aircraft orientation are described herein. One device includes instructions executable to determine a subsection of a rendering of a portion of an airport, wherein the subsection is associated with a particular stand of the airport, and wherein the subsection includes a plurality of ground travel pathways, determine a first subset of the plurality of pathways, a second subset of the plurality of pathways, and a third subset of the plurality of pathways, track a location of an outbound aircraft within the subsection of the rendering, determine an orientation of the aircraft according to a first set of rules responsive to a determination that the location of the aircraft is within the first or second subset of the plurality of pathways, and determine the orientation of the aircraft according to a second set of rules responsive to a determination that the location of the aircraft is within the third subset of the plurality of pathways.

Abstract: A task management system of an aircraft crew during a mission includes a task sequencing module configured to acquire a first list of procedure tasks for normal and special missions to be performed during the mission, a second list of abnormal, emergency and deferred procedure tasks, to be performed in case of defect and/or failures, and a third list of additional tasks resulting from entries by the crew. The task sequencing module is configured for defining a priority order and/or a planning order between the tasks to be performed immediately from among the tasks of the first list, the second list and the third list. The display management assembly is configured to display a first overall task sequencing window including tasks from the first list, the second list and the third list ranked according to the priority order and/or according to the planning order.

Abstract: Methods are provided for adjusting any correlation between a perspective of an onboard visual display and a current orientation of an inflight aircraft. The method comprises determining the current orientation of the inflight aircraft and determining the perspective of the visual display. The visual display is shown to a pilot of the inflight aircraft on a display element located onboard the inflight aircraft. The current orientation of the aircraft is compared with the perspective of the visual display to determine if the perspective of the visual display needs to transition to reflect the current orientation of the aircraft. If the display does need to be changed, a rate of transition of the visual display's perspective is selected based on current aircraft performance parameters. The perspective of the visual display is then transitioned to reflect the current orientation of the aircraft at the selected rate.

Abstract: Systems and methods for changing the orientation of information displayed on a display device mounted on a control pedestal at a position between two seats. One method involves changing the orientation of information displayed on a display device located on a control pedestal of an aircraft so that, instead of sub-optimal joint viewing of the displayed information by two pilots, an individual pilot may be able to read the displayed information more easily. The system enables either pilot to select a respective more optimal orientation for the displayed information for individual viewing. Each pilot may separately then quickly switch the display mode back to the “up is forward” orientation for joint viewing. Returning to the “up is forward” orientation may also be set to occur as a function of time.

Abstract: Systems and methods for collecting weather information for selected airspace regions are provided. In one embodiment, a method for collecting weather information for selected airspace regions comprises: receiving aircraft position information for a plurality of aircraft; forming an aircraft weather group based on flight path attributes derived from the aircraft position information; selecting at least a first representative aircraft from the weather group; and receiving at a weather information ground station, weather data from one or more representative aircraft of the aircraft weather group, wherein only the one or more representative aircraft transmit weather information to the weather information ground station from the aircraft weather group.

Abstract: An enhanced flight management system and flight management method directed to improved guidance in unstable approach scenarios. The method includes receiving and processing a published arrival procedure (PAP), a published glide path (PGP), landing parameters, and real-time aircraft sensor data to determine a an actual approach profile, and whether the aircraft is following the reference approach profile. Approach stabilization criterion are determined, including, (i) a wind corrected air mass flight path angle (WC FPA) at the IMC; (ii) a vertical speed at the wind corrected air mass flight path angle (VS IMC); (iii) a wind corrected air mass flight path (WC FPA) angle at the VMC; and (iv) a vertical speed at the wind corrected air mass flight path angle (VS VMC). The method also determines whether an IMC criterion profile and a VMC criterion profile stabilizes the actual approach.

Abstract: A control system including a control device, which is connected to a power storage device capable of supplying power to one or more electric apparatuses, and a server, by which reduction in a communication load and appropriate charge/discharge control are both achieved, is provided. When acquiring weather information from a server, a control device, on the basis of the weather information, charge to the power storage device and power supply from the power storage device to the electric apparatus. The control device decides a period from timing at which the weather information is acquired to timing at which weather information is next acquired. At second timing at which the period has elapsed from first timing at which the weather information has been acquired, the control device repeats an operation from acquisition of weather information to decision of a period after which weather information is next acquired from the server.

Abstract: Systems and methods for time-based viewing of clearance requests are provided. The system generates a time scale of substantially a same width as a displayed lateral image and renders the time scale on a periphery of the lateral image. The system receives a recommended change to an active trajectory from one or more on-board avionics or external sources, and then time-tag processes the recommended change to predict a clearance request and its associated relevant time. The system is configured to receive a user selected future time for viewing clearance requests. Responsive to the user selected future time, the system determines that the predicted clearance request is relevant at the future time, formats the predicted clearance request as a downlink message (DM), and renders, on the time scale, the formatted predicted clearance request alongside a symbolic indicator at the future time.

Abstract: Systems and methods directed to improvements in the presentation of CAVS procedures on an aircraft display system over what is conventionally available are provided. The provided systems and methods employ a vertical situation display (VSD), thereby presenting additional relevant visual approach information, such as a vertical distance between the ownship and the target aircraft, descent rates of the ownship and the target and an alerting function for the user-selected CAVS range. The provided systems and methods also capably receive and process user selections of target aircraft from both the lateral display and the VSD.

Abstract: A system and method for mapping an aircraft position on segments that lie between waypoints on a non-linear map by converting real world geographic coordinates of an aircraft to image X, Y coordinates using an image X, Y length or scale of a respective segment as a basis for the conversion. The aircraft position may be mapped in real time and presented to a user via an aircraft device.

Abstract: A flight planning system is disclosed for providing an interactive and customizable flight planning tool. The flight planning system may include a memory device for storing flight information and one or more hardware processors. The processors may receive, from a client device associated with the flight planning system, a first flight information request and provide, in response to the first flight information request, an interactive user interface having a graphical representation of a flight plan that includes at least a flight route. The processors may provide a plurality of selectable overlays that modify the appearance of the graphical representation and display additional information related to the flight information. The processors may receive a second request related to the flight information and provide a modified user interface comprising at least a feature related to the second request and the flight information.

Abstract: A computer system to continuously maintain a user session when a display device is mechanically connected and disconnected with a base processing device is described. The computer system allows the user to run applications during the user session on the base processing device and use the display device as a monitor. The display device can be detached from the base processing device, and the base processing device can continue running the applications for the user session. In this mode, the separated display device can be used as a tablet form factor computing device which can accept user input and send the user input to the base processing device. Among other functions, the base processing device can operate with the display device disconnected by generating session content for the display device, including, for example, sending application content, video streams, and other content to the display device.

Abstract: Systems and methods for an enhanced computer vision module are presented. The system receives host locating information, and determines a position and a location of the host based on the host locating information. The system determines a field of view (FOV) of the host based on the host locating information, and controls a camera associated with the host that is configured to record a video stream comprising the FOV. The system and method provide an improvement over conventional computer vision (CV) systems by utilizing object locating information that is transmitted, and also by keeping a storage table of learned and fixed objects. The provided system and method improve the efficiency of object recognition and computer aided maintenance (CAM).

Abstract: Methods are provided for adjusting any correlation between a visual display perspective and a default display view of an aircraft. The method comprises determining the default display view for an inflight aircraft and determining the orientation of the visual display for the crew of the aircraft. The default display view is compared with the orientation of the visual display to determine if the visual display's perspective needs to be transitioned to reflect the default display view. If the display does need to be changed, the rate of transition of the visual display's perspective is selected based on current aircraft performance parameters.

Abstract: Provided are methods, devices, and non-transitory computer-readable storage mediums to generate an itinerary with a weather forecast. The itinerary may comprise a departure location, a destination location and a first time. Based on the itinerary, an intermediary location and an intermediary time associated with the intermediary location may be identified. A weather forecast associated with the identified intermediary location and the intermediary time may be predicted. A weather risk associated with the identified route may be assessed and. based on the assessed risk, an alternative route may be additionally identified.

Abstract: A system and method for an interactive avionics display system integrates a large-format primary avionics display, a secondary avionics display capable of mirroring the display of electronic flight bag mobile devices, a format selector panel, and a keyboard panel. Background displays and foreground multifunction windows generated by the display system house applications and display relevant avionics data. The multifunction windows can be resized or repositioned on the display surface using finger contacts and gestures. Format selector panels include control selectors corresponding to the multifunction windows, the control selectors responsive to finger contact with the format selector panels or the corresponding multifunction windows. Keyboard panels provide touch-sensitive radio and communications controls as well as an alphanumeric keyboard responsive to finger contact with text fields generated by the display.

Abstract: A method for adapting an aircraft constant-gradient descent segment comprises: an acquisition step in which state variables characterizing the aircraft, environment variables characterizing the environment thereof and path variables characterizing the predicted path thereof at one of the initial and final points of the segment are acquired; a calculation step whereby a limit ground gradient for at least one performance criterion is calculated from the state variables, environment variables and path variables; a validity verification step checking the validity of the path initially predicted against the most restrictive limit ground gradient; and when the path initially predicted is not valid: a feasibility verification step checking the feasibility of a command to modify at least one state variable; if feasibility is verified, a prediction of executing the command; otherwise, a prediction of modifying one of the initial and final points of the segment with respect to constraints of the flight plan.

Abstract: A driving assistance device including means for determining a target speed, means for comparing an instantaneous speed of the railway vehicle with the target speed or with an interval around the target speed, and means for displaying driving instructions intended for a conductor of the railway vehicle, the driving instructions including instructions for modifying the instantaneous speed in order to bring it closer to the target speed, the display means being configured to: display a speed increase instruction icon when the instantaneous speed is below a first predetermined value, and to display a speed decrease instruction icon when the instantaneous speed is above a second predefined value.

Abstract: This disclosure is directed to an automated aerial vehicle (“AAV”) and systems, devices, and techniques pertaining to canceling noise, generating audible communications, and/or generating visible communications. The AAV may include one or more propellers utilized, in part, to produce sound that cancels noise generated by one or more other propellers. Additionally or alternatively, the AAV may utilize one or more propellers to generate audible and/or visible communications.

Abstract: An in-vehicle information display device has a first display and a second display disposed in a vehicle interior, a display content determination unit configured to determine whether a first content displayed on the first display and a second content displayed on the second display are identical to each other, and a display content change unit. When the display content determination unit determines that the first and second contents are identical to each other, the display content change unit changes the first content displayed on the first display or the second content displayed on the second display to a third content associated beforehand with one of the first and second contents that have been determined to be identical.

Abstract: Architecture having an algorithm that computes visible structures for a user within a distance defined by one or more environmental conditions. An environmental condition such as reduced visibility due to a weather condition such as rain, fog, etc., can be used to define a radius about the user in which possible points of interest (POIs) can be identified as viewable based on current weather visibility data. The altitude of the user is considered when identifying the possible POIs. The user is more likely capable of viewing other structures as POIs when the user is at a higher altitude. If the user is known to be standing on a ridge overlooking a city, this information can be processed by the algorithm to then show more POIs relative to this elevated user location than if the user was at approximately zero altitude. A sight map is generated based on these considerations.

Abstract: A method includes receiving meteorological forecast data at an electronic device. The method includes predicting multiple risk levels associated with an aircraft using one or more runways of an airport during a forecast time interval based on the meteorological forecast data. The method further includes generating a graphical user interface (GUI) that includes multiple risk indicators based on the multiple risk levels. The multiple risk indicators may correspond to multiple time sub-intervals during the forecast time interval.

Abstract: Described herein are systems and methods for tracking suspect aircraft. One embodiment is related to a method including receiving location data and current flight data of an aircraft, analyzing the location data and current flight data using flight behavior algorithms, detecting route deviation of the aircraft, and providing a report of flight pattern analysis and the detected route deviation to at least one device on a network.

Abstract: A system and method for providing visual depictions of a predictive weather forecast for in-route vehicle trajectory planning. The method includes displaying weather information on a graphical display, displaying vehicle position information on the graphical display, selecting a predictive interval, displaying predictive weather information for the predictive interval on the graphical display, and displaying predictive vehicle position information for the predictive interval on the graphical display, such that the predictive vehicle position information is displayed relative to the predictive weather information, for in-route trajectory planning.

Abstract: A navigation device is provided that includes a processor configured to track a path of the navigation device based on a first signal received by the navigation device, and calculate a calculated position of the navigation device based on a second signal different from the first signal. The navigation device may further include a graphical user interface configured to display a calculated position graphical element representing the calculated position determined based on the second signal and display a tracked position graphical element representing the path of the navigation device determined based on the first signal, the tracked position graphical element and the calculated position graphical element being distinguishable in appearance.

Abstract: The present disclosure is generally directed to a method of generating and displaying a parachute flare drift vector symbol on a navigation display of the aircraft capable of deploying a flare relative to a real-time navigation map. The flare drift vector symbol includes a flare ignition forward/aft distance relative to the aircraft deploying the flare, a flare ignition left/right distance relative to the aircraft deploying the flare, a flare burn vector distance, and a flare burn vector direction. The flare drift vector symbol is generating based on the flare parameters, the wind parameters, the flare drift distance, the flare drift direction and the aircraft parameters.

Abstract: The system includes additional display means including at least one additional screen and additional graphic interface handling means of the additional screen (able to display on the additional screen, a summary window depending on the operational state of the aircraft. The summary window comprises at least one first pictogram able to be displayed on a first display window of main display means of the aircraft without being displayed on the second window of the main display means, and at least one second pictogram intended to be displayed on the second display window of the main display means without being displayed on the first window of the main display means.

Abstract: Disclosed are methods and systems of rapidly validating accuracy in particle cloud forecast transport and dispersion models. An example method can comprise accessing a forecast model of a volcanic ash cloud. An example method can comprise generating first data based at least on the forecast model. The first data can have at least one fewer spatial dimension than second data associated with the forecast model. An example method can comprise determining accuracy of the forecast model based at least on measurements of at least a portion of the volcanic ash cloud. An example method can comprise refining the forecast model based at least on the determined accuracy, thereby improving a representation of the volcanic ash cloud.

Abstract: A method includes receiving visual flight rules (VFR) data and determining a suggested path of approach for an aircraft based on the VFR data. The suggested path of approach may correspond to a flight path of the aircraft to a runway of an airport. The method includes highlighting a representation of the suggested path of approach at a display device.

Abstract: This disclosure is directed to devices, systems, and methods for enabling and operating an onboard weather display system with managed bandwidth. In one example, a method includes receiving, by a hub system, initial sets of data from one or more aircraft. The method further includes receiving secondary sets of data from the aircraft, wherein the secondary sets of data are related to a significant weather condition. The method further includes transmitting an initial data stream to a particular aircraft, wherein the initial data stream is based at least in part on the initial sets of data from the one or more aircraft. The method further includes transmitting, in response to a request from the particular aircraft, a secondary data stream based at least in part on the secondary sets of data related to the significant weather condition.

Abstract: A method of operating an aircraft comprising a cockpit with a flight deck having at least one flight display, a pilot's seat facing the flight deck, and a synthetic vision system producing a synthetic image for displaying on the at least one flight display.

Abstract: This relates to a method and device for constructing a vertical profile for an aircraft descent and/or approach. The construction device comprises a data-capture unit configured to provide, for at least one of a plurality of parameters, a value relating to a user strategy. A construction unit is configured to automatically construct a vertical profile for an aircraft descent and/or approach, using the value thus provided.

Abstract: Systems, apparatus, and methods for controlling power modes in electronic devices are provided. A system may include an electronic device and an input device that sends power mode selection information via a network to a power mode selection receiving component in the electronic device. The electronic device includes a first power component that powers a first component, and a switching component that controls the first power component. The electronic device may include a second power component that powers a second component. The switching component may control the second power component. The power mode selection receiving component and the switching component may be powered independently of the first and the second component. If the power mode selection information indicates an off mode, the electronic device may provide power to the power mode selection receiving component and the switching component and not to the first and the second component.

Abstract: An aircraft cockpit display arrangement having a primary instrument display region for positioning in front of at least one pilot. The primary instrument display region has a wide screen format panel display and duplicated redundant display drive electronics configured to present both primary flight information and navigational display information on the same screen.

Abstract: A computing unit allocates boarding paths, available for boarding a transport unit, in particular an aircraft, to passengers of the transport unit. An associated method allocates boarding paths, available for boarding the transport unit to passengers of the transport unit. A computer program carries out the method, and a directing system directs passengers of the transport unit along boarding paths available for boarding the transport unit. The computing unit is configured to form two or more changeable seat groups from a plurality of seats provided in the transport unit and to allocate the boarding paths, available for boarding the transport unit, to the two or more seat groups formed.

Abstract: The present invention relates to a method and system for displaying multiple aircrafts positions in a display system for real-time monitoring flights. The method will enables the trainer in the ground station, to select and to switch between aircrafts to monitor the flight at real time as if he were next to the selected trainee and to see the instruments panel and also the three dimensional positions of the respective aircraft as seen from the cockpit and to conduct a conversation with the pilot. The method enable to give to the trainee the needed instructions to overcome problem he might face during flight and to displays a warning mark when a distance between two aircraft is shorter than a threshold value and. The method enables data transmission based on a cellular internet communication.

Abstract: A system and method are described for receiving a NOTAM and storing information relating to the distance of a temporarily displaced threshold for a runway. When that runway is selected for approach and landing, the temporarily displaced threshold and new aiming point are automatically displayed. The change made to the display using NOTAM data can be indicated to the pilot by distinct symbology or particular color, or by using an icon or an annunciation.

Abstract: A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.

Abstract: A method of creating at least one flight plan of an aircraft includes entering a creation objective which illustrates a type and general characteristics of the flight plan to be created, automatically generating a flight plan outline, automatically generating a targeted request for information relating to missing parameters, entering the requested information relating to the missing parameters, and supplementing automatically the flight plan outline and automatically deleting any discontinuities to create, in a definitive manner, the flight plan.

Abstract: Gaze based systems and methods are used to aid traffic controllers and/or pilots. A gaze line of an eye of the user viewing the display is tracked using an eyetracker. An intersection of the gaze line of the eye with the display is calculated to provide continuous feedback as to where on the display the user is looking. A trace of the gaze line of the eye is correlated with elements of a situation. The user's awareness of the situation is inferred by verifying that the user has looked at the elements of the situation. In an embodiment, the user is notified of the situation when it is determined that the user has not looked at the elements of the situation for a predetermined period of time. The notification is automatically removed once it is determined that the user has looked at the elements of the situation.