SITUATION-AWARE, INTELLIGENT DATA-SYNCHRONIZATION METHODS FOR UAV-INSPECTION APPLICATIONS

    公开(公告)号:US20220013015A1

    公开(公告)日:2022-01-13

    申请号:US17019029

    申请日:2020-09-11

    Abstract: Unmanned aerial vehicle (UAV) systems are described that determine when to automatically transfer telemetry data from a UAV to a ground-based computing device by monitoring one or more context states of the UAV. In some examples, a UAV system includes a UAV; a ground-based computing device; and processing circuitry configured to acquire data from one or more sensors on the UAV; store the data at a local storage device on the UAV; maintain a state machine configured to monitor one or more context states of the UAV system; determine, based on the one or more context states, that a current situation of the UAV system meets minimum criteria for transferring the data from the UAV to the ground-based computing device; and automatically transfer, based on the determination, the data from the UAV to the ground-based computing device.

    SYSTEMS, APPARATUSES, METHODS, AND COMPUTER PROGRAM PRODUCTS FOR MOTION STABILIZED TOUCH CONTROL

    公开(公告)号:US20250138675A1

    公开(公告)日:2025-05-01

    申请号:US18922076

    申请日:2024-10-21

    Abstract: Embodiments of the present disclosure provide techniques for motion stabilized touch control. Reference data comprising one or more stabilized positions for one or more touch points corresponding to one or more touch zones associated with a touch screen device may be generated using a motion stabilization model. One or more touch zones may be adjusted based on the stabilized positions by transmitting-computer executable-instructions configured to cause the one or more touch zones to be aligned with the one or more stabilized positions. One or more touch detection models associated with the touch screen device may be updated by tuning the one or more touch detection models to learn the stabilized positions. One or more dimensions of the one or more touch zones may be recalibrated by adjusting a size of at least one of the one or more touch zones.

    INTEGRATED FLIGHT DECK
    4.
    发明公开

    公开(公告)号:US20240194080A1

    公开(公告)日:2024-06-13

    申请号:US18174553

    申请日:2023-02-24

    CPC classification number: G08G5/0021 G06Q10/047 G06Q30/04 G08G5/0034

    Abstract: A system for an aircraft configured to: provide one or more of the sensed aircraft characteristics to a flight planning tool for processing by one or more features of the flight planning tool; receive a recommended flight setting from the flight planning tool based on the processing by the flight planning tool; compare a current flight setting as determined based on the one or more sensed aircraft characteristics from the plurality of sensors with the received recommended flight setting; determine a potential operational efficiency based on the comparison between the received recommended flight setting and the current flight setting; and provide the potential operational efficiency to a user based on an identity of the user.

    DYNAMIC FLIGHT OPERATION OPTIMIZATION

    公开(公告)号:US20240404414A1

    公开(公告)日:2024-12-05

    申请号:US18644204

    申请日:2024-04-24

    Abstract: Techniques for generating flight operation recommendation for an aircraft are described. In operation, a flight safety hazard is detected on a flight path corresponding to a current flight operation of an aircraft. In response, the current flight operation is modified to generate a modified flight operation. A plurality of avionics parameters is then obtained from avionics systems available onboard the aircraft. A variation in the flight safety hazard is then detected based on at least one avionics parameter from the plurality of avionics parameters. Upon ascertaining the variation to be detrimental to the modified flight operation of the aircraft, the plurality of avionics parameters is analysed using a flight operation recommendation model to generate a plurality of flight operation recommendations. A flight operation recommendation from the plurality of flight operation recommendations is then applied to the modified flight operation.

    SYSTEMS AND METHODS FOR CONTEXT-BASED COCKPIT SIMULATION

    公开(公告)号:US20240194089A1

    公开(公告)日:2024-06-13

    申请号:US18172503

    申请日:2023-02-22

    CPC classification number: G09B9/165 G08G5/0021

    Abstract: A system includes a communication device, a display, an input/output interface, a processing device, and a memory, storing one or more instructions that cause the system to: receive electronic flight book (EFB) selection information for selecting one EFB GUI from a plurality of selectable EFB GUIs that provide an interface for entry and display of flight information; select one EFB GUI from the plurality of selectable EFB GUIs based on the received EFB selection information; display the selected EFB GUI on the display; receive one or more flight parameters from a flight management system (FMS); display one or more of the one or more flight parameters on the displayed EFB GUI; receive one or more changes to the one or more flight parameters via the input/output interface; and update one or more of the one or more flight parameters in the FMS based on the received one or more changes.

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