GEO-FIDUCIALS FOR UAV NAVIGATION
    3.
    发明申请

    公开(公告)号:US20200301445A1

    公开(公告)日:2020-09-24

    申请号:US16360952

    申请日:2019-03-21

    申请人: WING Aviation LLC

    摘要: Unmanned aerial vehicle (UAV) navigation systems include a UAV charging pad positioned at a storage facility, a plurality of fiducial markers positioned at the storage facility, and a UAV. Each fiducial marker is associated with a fiducial dataset storing a position of the fiducial marker, and each fiducial dataset is stored in a fiducial map. The UAV has a navigation system that includes a camera, a fiducial navigation sub-system, a non-fiducial navigation sub-system, and logic that when executed causes the UAV to image a first fiducial marker with the camera, to transition from a non-fiducial navigation mode to a fiducial navigation mode, to access from the fiducial map the fiducial dataset storing the position of the first fiducial marker, and to navigate based upon the fiducial dataset storing the position of the first fiducial marker, into alignment with and land on the UAV charging pad.

    Systems and methods for stopping movement of operational members

    公开(公告)号:US11370555B2

    公开(公告)日:2022-06-28

    申请号:US16729167

    申请日:2019-12-27

    申请人: Wing Aviation LLC

    摘要: A method is provided that includes causing an operational member of a system to move. The method includes driving a power or control signal through a conductive coupling member. The conductive coupling member is connected between a first terminal and a second terminal in a power circuit, and the coupling member secures the operational member to a structural member of the system. The method includes detecting an electrical disconnect between the first terminal and a second terminal. The method includes determining a mechanical break associated with the coupling member based on the electrical disconnect between the first terminal and the second terminal. The method includes causing the operational member of the system to stop moving based on determining the mechanical break associated with the coupling member.

    Geo-fiducials for UAV navigation
    7.
    发明授权

    公开(公告)号:US11287835B2

    公开(公告)日:2022-03-29

    申请号:US16360952

    申请日:2019-03-21

    申请人: WING Aviation LLC

    摘要: Unmanned aerial vehicle (UAV) navigation systems include a UAV charging pad positioned at a storage facility, a plurality of fiducial markers positioned at the storage facility, and a UAV. Each fiducial marker is associated with a fiducial dataset storing a position of the fiducial marker, and each fiducial dataset is stored in a fiducial map. The UAV has a navigation system that includes a camera, a fiducial navigation sub-system, a non-fiducial navigation sub-system, and logic that when executed causes the UAV to image a first fiducial marker with the camera, to transition from a non-fiducial navigation mode to a fiducial navigation mode, to access from the fiducial map the fiducial dataset storing the position of the first fiducial marker, and to navigate based upon the fiducial dataset storing the position of the first fiducial marker, into alignment with and land on the UAV charging pad.

    Systems and Methods for Stopping Movement of Operational Members

    公开(公告)号:US20210197977A1

    公开(公告)日:2021-07-01

    申请号:US16729167

    申请日:2019-12-27

    申请人: Wing Aviation LLC

    IPC分类号: B64D27/24 B64C39/02 B64C27/68

    摘要: A method is provided that includes causing an operational member of a system to move. The method includes driving a power or control signal through a conductive coupling member. The conductive coupling member is connected between a first terminal and a second terminal in a power circuit, and the coupling member secures the operational member to a structural member of the system. The method includes detecting an electrical disconnect between the first terminal and a second terminal. The method includes determining a mechanical break associated with the coupling member based on the electrical disconnect between the first terminal and the second terminal. The method includes causing the operational member of the system to stop moving based on determining the mechanical break associated with the coupling member.

    Systems and methods for autonomous airworthiness pre-flight checks for UAVs

    公开(公告)号:US11912432B2

    公开(公告)日:2024-02-27

    申请号:US17118530

    申请日:2020-12-10

    申请人: Wing Aviation LLC

    IPC分类号: B64C39/02 B64D45/00 G08G5/00

    摘要: A method includes determining an operational condition associated with an unmanned aerial vehicle (UAV). The method includes, responsive to determining the operational condition, causing the UAV to perform a pre-flight check. The pre-flight check includes hovering the UAV above a takeoff location. The pre-flight check includes, while hovering the UAV, moving one or more controllable components of the UAV in accordance with a predetermined sequence of movements. The pre-flight check includes obtaining, by one or more sensors of the UAV, sensor data indicative of a flight response of the UAV to moving the one or more controllable components while hovering the UAV. The pre-flight check includes comparing the sensor data to expected sensor data associated with an expected flight response to the predetermined sequence of movements while hovering the UAV. The pre-flight check includes, based on comparing the sensor data to the expected sensor data, evaluating performance of the UAV.