DRONE INTEGRATED CONTROL DEVICE
    21.
    发明公开

    公开(公告)号:US20240140624A1

    公开(公告)日:2024-05-02

    申请号:US18406214

    申请日:2024-01-08

    申请人: Ha Na LEE

    IPC分类号: B64U20/80 G05D1/86

    摘要: A drone integrated control device that controls a drone by unifying respective components on one board includes a flight control unit including a plurality of sensors and configured to control a path and a flight attitude of the drone, a motor control unit configured to control a rotation speed of at least one motor mounted to perform movements and takeoffs of the drone, a communication unit configured to transmit and receive control signals input to and output from the respective components included in the drone integrated control device, and a power supply unit configured to supply power to the respective components included in the drone integrated control device to operate the respective components.

    UNMANNED SYSTEM MANEUVER CONTROLLER SYSTEMS AND METHODS

    公开(公告)号:US20230359226A1

    公开(公告)日:2023-11-09

    申请号:US18344753

    申请日:2023-06-29

    申请人: KNIGHTWERX INC.

    摘要: An unmanned system maneuver controller (USMC) includes an inertial navigation system (INS) for state estimation of the USMC in three-dimensional (3D) space, a communications device configured to communicate with an unmanned system, and a processor configured to receive, via the communications device, flight, maneuver, or dive data from the unmanned system, and generate flight, maneuver, or dive control instructions based at least on the flight, maneuver, or dive data and data received from the INS. The flight, maneuver, or dive control instructions are configured to pilot the unmanned system based on movement of the USMC in 3D space. A remote may selectively control an operation of the USMC. The USMC may be mounted to a weapon or observation device, such that movement of the weapon or observation device in 3D space controls a movement of the unmanned system. Additional systems and associated methods are also provided.

    Off-Channel Unmanned Aerial Vehicle Remote ID Beaconing

    公开(公告)号:US20230294848A1

    公开(公告)日:2023-09-21

    申请号:US18124527

    申请日:2023-03-21

    申请人: Skydio, Inc.

    IPC分类号: B64U20/80

    摘要: Provided herein are various enhancements for unmanned aerial vehicles and operations. An unmanned aerial vehicle includes a wireless communication system configured to establish a wireless link for at least flight control information for the unmanned aerial vehicle. The wireless communication system is configured to monitor the flight control information using a first wireless channel having a first bandwidth and periodically tune away to a second wireless channel having a second bandwidth wider than the first bandwidth for transmission of a beacon frame that includes remote identification information corresponding to the unmanned aerial vehicle.

    COMMUNICATION DEVICE AND METHOD, AND UNMANNED AERIAL VEHICLE EMPLOYING THE SAME

    公开(公告)号:US20230254005A1

    公开(公告)日:2023-08-10

    申请号:US18101775

    申请日:2023-01-26

    摘要: The present disclosure provides a communication device which is suitable for use in an unmanned aerial vehicle operating in an unmanned aerial vehicle collaboration system including multiple unmanned aerial vehicles and enables both a data communication with another unmanned aerial vehicle and a measurement of a distance to another unmanned aerial vehicle. According to an aspect of an exemplary embodiment, a communication device of an unmanned aerial vehicle includes: an ultra-wideband (UWB) communication circuit configured to perform a UWB communication with other unmanned aerial vehicle; and a UWB communication manager configured to send transmit data to the other unmanned aerial vehicle and receive data sent by the other unmanned aerial vehicle through the UWB communication circuit, and transmit or receive shared data to be shared by unmanned aerial vehicles in a form of being appended to a distance measurement frame.

    UNMANNED AIRCRAFT
    27.
    发明公开
    UNMANNED AIRCRAFT 审中-公开

    公开(公告)号:US20230234730A1

    公开(公告)日:2023-07-27

    申请号:US18002276

    申请日:2021-06-16

    发明人: Yosuke MATSUZAKI

    摘要: The present disclosure relates to an unmanned aircraft capable of suitably limiting a variation in pressure altitude.
    The unmanned aircraft includes a housing that constitutes a main body, one barometric pressure sensor that is provided in one space formed inside the housing, and four or more openings that have substantially the same opening area, the four or more openings being arranged in a balanced manner over an entire circumference of a side portion of the housing. The present disclosure can be applied to a drone including a barometric pressure sensor.

    SPHERICAL DRONE AND CONTROL METHOD THEREOF
    28.
    发明公开

    公开(公告)号:US20240343422A1

    公开(公告)日:2024-10-17

    申请号:US18313497

    申请日:2023-05-08

    申请人: GANG YAO

    发明人: GANG YAO

    摘要: A spherical drone and a control method thereof relate to a field of drones. The spherical drone includes a main shell defines an accommodating space, an inner support arranged in the accommodating space, a main control board, a power supply, a motor, a fixing shaft, an upper blade and an lower blade rotatably arranged on the fixing shaft, and a first crown gear and a second crown gear arranged on the inner support. Slotted holes are defined on the main shell. The first crown gear and the second crown gear are sleeved on the fixing shaft. The upper blade is fixed on the first crown gear. The lower blade is fixed on the second crown gear. The motor drives the first crown gear and the second crown gear to rotate, so as to simultaneously drive the upper blade and the lower blade to rotate.