AERIAL VEHICLE AND CONTROL METHOD AND APPARATUS THEREFOR, AND STORAGE MEDIUM

    公开(公告)号:US20240199219A1

    公开(公告)日:2024-06-20

    申请号:US18430678

    申请日:2024-02-02

    CPC classification number: B64D31/06 B64C27/26 G05D1/49 G05D2109/254

    Abstract: A controller for an aerial vehicle, the aerial vehicle comprising a fuselage, fixed wings, and a multi-rotor assembly, the fixed wings disposed on both sides of the fuselage, and the multi-rotor assembly comprising at least two rotors disposed on either the fuselage or the fixed wings. The controller may comprise at least one memory storing at least one instruction set configured to control the vehicle, and at least one processor, communicatively coupled to the at least one memory. When the aerial vehicle operates, the at least one processor executes the at least one instruction set to, during cruise of the aerial vehicle, control at least a portion of the rotors of the multi-rotor assembly to actively rotate to provide a force in a vertical direction so that the multi-rotor assembly and the fixed wings together provide lift for the aerial vehicle.

    UNMANNED AERIAL VEHICLE CONTROL METHOD, AND UNMANNED AERIAL VEHICLE

    公开(公告)号:US20210208609A1

    公开(公告)日:2021-07-08

    申请号:US17206105

    申请日:2021-03-18

    Inventor: Yang LI Chen CHEN

    Abstract: A method for controlling an unmanned aerial vehicle includes generating a course reversal command to control the unmanned aerial vehicle to execute a course reversal action. The course reversal action includes at least a cruising stage. The method further includes, in the cruising stage, measuring one or more flight parameters of the unmanned aerial vehicle and controlling the unmanned aerial vehicle to enter a high wind course reversal stage in response to determining that the unmanned aerial vehicle is in a high wind retardant state according to the one or more flight parameters. The method also includes, in the high wind course reversal stage, measuring the one or more flight parameters, and controlling the unmanned aerial vehicle to return to the cruising stage in response to determining that the unmanned aerial vehicle is not in the high wind retardant state according to the one or more flight parameters.

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