DRONE ADAPTER FOR DROPPING SPOON-BASED DEVICES

    公开(公告)号:US20250066019A1

    公开(公告)日:2025-02-27

    申请号:US18237184

    申请日:2023-08-23

    Abstract: A system and method allowing spoon-based devices to be carried and dropped by a drone. The preferred embodiments are adapted for use with a drone having a retracting drop shaft release mechanism. First and second adapter portions are provided. These clamp around the body of a spoon-based device and hold the spoon-based device. The lower regions of the first and second adapter portions are joined by a pivot joint. The upper regions each include an engagement feature such as an upstanding tang portion. These first and second tang portions are engaged to the drone's release unit.

    Localization analytics algorithms and methods

    公开(公告)号:US12216105B2

    公开(公告)日:2025-02-04

    申请号:US17251089

    申请日:2019-06-19

    Applicant: SeekOps Inc.

    Abstract: Systems, devices, and methods for receiving, by a ground control station (GCS) having a processor with addressable memory, a plurality of point source gas concentration measurements; receiving, by the GCS, a meteorological data corresponding to each point source concentration gas measurement; determining, by the GCS, if each point source gas concentration measurement is an elevated ambient gas concentration; generating, by the GCS, a back trajectory for each elevated ambient gas concentration; storing, by the GCS, the position of each generated back trajectory in a grid; determining, by the GCS, a probability of a gas source location corresponding to the stored positions in the grid; and generating, by the GCS, an overlay showing the probability of the gas source location.

    OMNIDIRECTIONAL PROPELLED VEHICLE COMPRISING A FIRST ROTARY SHAFT

    公开(公告)号:US20250019098A1

    公开(公告)日:2025-01-16

    申请号:US18849330

    申请日:2023-03-21

    Applicant: AERIX SYSTEMS

    Abstract: The invention relates to a propelled vehicle (D1; D2) comprising: an electrical power source (SE), a chassis (C), a first shaft (A1) supporting a propulsion unit (P) and mounted such that it can rotate on the chassis about a first axis (AX1), and a first device (E1) for rotating the first shaft, characterized in that the chassis comprises a first member (OGR1) for guiding the first shaft in rotation, in that the first shaft comprises a first complementary member (OC1) mechanically cooperating with the first guide member, and in that the first guide member and the first complementary member are electrically conductive and are electrically connected to one another, the first guide member being electrically connected to the electrical power source and the first complementary member being electrically connected to the propulsion unit.

    AIRCRAFT
    7.
    发明申请
    AIRCRAFT 有权

    公开(公告)号:US20240417114A1

    公开(公告)日:2024-12-19

    申请号:US18691352

    申请日:2022-09-13

    Abstract: Described is an aircraft, in particular a drone, with a supporting body (2) and at least two propulsion arrangements (4, 8) arranged at a distance from one another on the supporting body (2), which are designed to generate a propulsive thrust in a direction of propulsion (8b). According to a first aspect of the invention, the propulsion arrangements (4, 8) on the supporting body (2) are each mounted so as to be pivotable independently of one another about a first axis of pivoting (6) extending at an angle to the direction of propulsion (8b) and a first actuating drive (10) is provided and designed to pivot the propulsion arrangements (4, 8) independently of one another about the first axis of pivoting (6). According to a second aspect of the invention, in which a trunk body (20) is provided, this trunk body (20) is mounted on the supporting body (2) so as to be pivotable about a second axis of pivoting (22) and a second actuating drive (24) is provided and designed to pivot the supporting body (2) relative to the trunk body (20).

    ADAPTIVE CONTROLLER FOR UNMANNED AIRCRAFT

    公开(公告)号:US20240409228A1

    公开(公告)日:2024-12-12

    申请号:US18677644

    申请日:2024-05-29

    Inventor: Philip Herlihy

    Abstract: Techniques for an unmanned ariel vehicle (UAV) having a closed-loop controller that is gain scheduled based on a trained machine learning model. The closed-loop controller could be a PID controller. Real-time data pertaining to the motor being controlled is input to the trained machine learning model. Examples of the real-time data includes, but is not limited to, motor current, motor voltage, and an estimate of motor thrust. The trained machine learning model may also input an error term of the closed-loop controller. Tuning constants for the closed-loop controller are derived based on the prediction from the machine learning model. Gain scheduling for the closed-loop controller may thus be performed “online” while the UAV continues on its mission. Controller gain scheduling may be performed to account for changes in a payload carried by the UAV.

    DEVICE AUTHENTICATION FOR WIRELESS CHARGING

    公开(公告)号:US20240408983A1

    公开(公告)日:2024-12-12

    申请号:US18674473

    申请日:2024-05-24

    Applicant: WiBotic Inc.

    Inventor: Benjamin Waters

    Abstract: An authentication between a wireless charger and a device configured to receive wireless energy from the wireless charger includes establishing a wireless data channel between the wireless charger and the device. An authentication challenge signal is driven onto a transmit charging coil of the wireless charger and a receive charging coil of the device is configured to receive the authentication challenge signal. The device sends an authentication response signal to the wireless charger based at least in part on the authentication challenge signal.

Patent Agency Ranking