CONTROL METHOD AND DEVICE
    1.
    发明申请

    公开(公告)号:US20250013248A1

    公开(公告)日:2025-01-09

    申请号:US18891941

    申请日:2024-09-20

    Abstract: A control method is provided, including: obtaining a current altitude of an aircraft, and determining a preset horizontal deviation threshold corresponding to the current altitude; obtaining a current horizontal deviation, wherein the current horizontal deviation is a horizontal deviation between a landing position and a current position of the aircraft; and determining a landing strategy of the aircraft based at least in part on a comparison between the current horizontal deviation and the preset horizontal deviation threshold.

    METHOD AND SYSTEM FOR CONTROLLING MOVEMENT OF MOVABLE DEVICES

    公开(公告)号:US20210291982A1

    公开(公告)日:2021-09-23

    申请号:US17339827

    申请日:2021-06-04

    Abstract: A method of controlling movement of a plurality of movable devices includes determining, by a processor, at least one of a first priority level or a first safety zone for a first movable device of the plurality of movable devices. The method also includes determining, by the processor, at least one of a second priority level or a second safety zone for a second movable device of the plurality of movable devices based on information relating to the second movable device. The method further includes generating, by the processor, a collision avoidance measure to avoid collision with the second movable device during movement based on at least one of the first priority level, the first safety zone, the second priority level, or the second safety zone.

    UNMANNED AERIAL VEHICLE CONTROL METHOD AND APPARATUS, AND UNMANNED AERIAL VEHICLE

    公开(公告)号:US20240126305A1

    公开(公告)日:2024-04-18

    申请号:US18534743

    申请日:2023-12-11

    CPC classification number: G05D1/667 B64U50/13 G05D1/48 B64U2101/45

    Abstract: The present application relates to a control method of an aerial vehicle. The aerial vehicle may comprise a propulsion structure for providing flight power and a spraying apparatus for spraying a material. The control method may comprise determining current target information of the aerial vehicle during a process of the aerial vehicle performing a spraying task, wherein the current target information indicates wind field strength of a downward pressure wind field generated by the propulsion structure; determining, based on the current target information, a desired relative flight altitude of the aerial vehicle corresponding to the current target information relative to the material being sprayed below the aerial vehicle; and controlling the aerial vehicle to fly toward the desired relative flight altitude.

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