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    Autonomous control techniques for avoiding collisions with cooperative aircraft
    1.
    发明授权
    Autonomous control techniques for avoiding collisions with cooperative aircraft 有权

    公开(公告)号：US12165532B1

    公开(公告)日：2024-12-10

    申请号：US17581518

    申请日：2022-01-21

    Applicant: WING AVIATION LLC

    Inventor： Kevin Jenkins ,  John Mooney ,  Louis Dressel ,  Kyle Julian

    IPC: G08G5/00 ,  B64U10/20 ,  B64U101/00 ,  G05D1/00 ,  G08G5/04

    Abstract: In some embodiments, a non-transitory computer-readable medium having logic stored thereon is provided. The logic, in response to execution by one or more processors of an unmanned aerial vehicle (UAV), causes the UAV to perform actions comprising receiving at least one ADS-B message from an intruder aircraft; generating a intruder location prediction based on the at least one ADS-B message; comparing the intruder location prediction to an ownship location prediction to detect conflicts; and in response to detecting a conflict between the intruder location prediction and the ownship location prediction, determining a safe landing location along a planned route for the UAV and descending to land at the safe landing location.

    Counter-rotating propellers for aerial vehicle
    2.
    发明授权
    Counter-rotating propellers for aerial vehicle 有权

    公开(公告)号：US11091260B2

    公开(公告)日：2021-08-17

    申请号：US16008464

    申请日：2018-06-14

    Applicant: Wing Aviation LLC

    Inventor： Kevin Jenkins ,  Jacob Huffman ,  Nicolas Renold ,  Cameron Fitchener

    IPC: B64C29/00 ,  B64C39/04 ,  B64C39/02 ,  B64D31/06 ,  G05D1/04 ,  G05D1/08

    Abstract: An aerial vehicle includes an airframe; vertical propulsion units, and a controller. The vertical propulsion units are mounted to the airframe and include propellers oriented to provide vertical propulsion to the aerial vehicle. The vertical propulsion units are physically organized in quadrants on the airframe with each of the quadrants including two or more of the vertical propulsion units. The controller is coupled to the vertical propulsion units to control operation of the vertical propulsion units. At least two of the vertical propulsion units in each of the quadrants are adapted to counter-rotate from each other during flight of the aerial vehicle.

    Systems and Methods for Stopping Movement of Operational Members
    3.
    发明申请
    Systems and Methods for Stopping Movement of Operational Members 有权

    公开(公告)号：US20210197977A1

    公开(公告)日：2021-07-01

    申请号：US16729167

    申请日：2019-12-27

    Applicant: Wing Aviation LLC

    Inventor： Kevin Jenkins ,  André Prager ,  Brandon Jones ,  John FitzSimons

    IPC: B64D27/24 ,  B64C39/02 ,  B64C27/68

    Abstract: 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.

    UAV Route Planning for Mitigating Traffic Encounters
    4.
    发明申请
    UAV Route Planning for Mitigating Traffic Encounters 有权

    公开(公告)号：US20250157342A1

    公开(公告)日：2025-05-15

    申请号：US18506921

    申请日：2023-11-10

    Applicant: Wing Aviation LLC

    Inventor： Kevin Jenkins ,  John Gordon Mooney ,  Anthony Robert Nannini

    IPC: G08G5/00 ,  G08G5/04

    Abstract: A method is disclosed. The method includes receiving data for one or more aircraft currently flying within an airspace. The received data for each of the one or more aircraft includes a current position and at least one aircraft parameter. Based on the current position and the at least one aircraft parameter, the method also includes determining an initial volume and a predicted future trajectory for each of the one or more aircraft. The method additionally includes determining, based on the predicted future trajectory and the initial volume, an extended volume for each of the one or more aircraft. The method further includes determining, based on the extended volume determined for each of the one or more aircraft, a composite extended volume space. The method includes planning a flight path for an unmanned aerial vehicle (UAV) through the airspace based on the composite extended volume space.

    Techniques for validating UAV position using visual localization
    6.
    发明授权
    Techniques for validating UAV position using visual localization 有权

    公开(公告)号：US12235369B2

    公开(公告)日：2025-02-25

    申请号：US17864031

    申请日：2022-07-13

    Applicant: WING Aviation LLC

    Inventor： Kevin Jenkins ,  Damien Jourdan ,  Jeremie Gabor

    IPC: G01S19/48 ,  G01S19/26 ,  G01S19/40

    Abstract: Systems and methods for validating a position of an unmanned aerial vehicle (UAV) are provided. A method can include receiving map data for a location, the map data including labeled data for a plurality of landmarks in a vicinity of the location. The method can include generating image data for the location, the image data being derived from images of the vicinity generated by the UAV including at least a subset of the plurality of landmarks. The method can include determining a visual position of the UAV using the image data and the map data. The method can include determining a Global Navigation Satellite System (GNSS) position of the UAV. The method can include generating an error signal using the visual position and the GNSS position. The method can also include validating the GNSS position in accordance with the error signal satisfying a transition condition.

    Systems and methods for autonomous airworthiness pre-flight checks for UAVs
    7.
    发明授权
    Systems and methods for autonomous airworthiness pre-flight checks for UAVs 有权

    公开(公告)号：US11912432B2

    公开(公告)日：2024-02-27

    申请号：US17118530

    申请日：2020-12-10

    Applicant: Wing Aviation LLC

    Inventor： Brandon Jones ,  Kevin Jenkins ,  Damien Jourdan ,  André Prager

    IPC: B64C39/02 ,  B64D45/00 ,  G08G5/00

    CPC classification number: B64D45/00 ,  B64C39/024 ,  G08G5/0013 ,  B64D2045/0085 ,  B64U2201/10 ,  B64U2201/20

    Abstract: 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.

    Systems and Methods for Autonomous Airworthiness Pre-Flight Checks for UAVs
    9.
    发明申请
    Systems and Methods for Autonomous Airworthiness Pre-Flight Checks for UAVs 有权

    公开(公告)号：US20220185499A1

    公开(公告)日：2022-06-16

    申请号：US17118530

    申请日：2020-12-10

    Applicant: Wing Aviation LLC

    Inventor： Brandon Jones ,  Kevin Jenkins ,  Damien Jourdan ,  André Prager

    IPC: B64D45/00 ,  B64C39/02 ,  G08G5/00

    Abstract: 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.

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