Aircraft, takeoff control method and system, and landing control method and system

    公开(公告)号:US11975818B2

    公开(公告)日:2024-05-07

    申请号:US17037231

    申请日:2020-09-29

    Inventor: Canlong Lin

    CPC classification number: B64C13/18 B64C39/024 B64D45/04 G05D1/0676 G05D1/10

    Abstract: A landing control method for an aircraft includes detecting whether a landing indication signal is received, controlling the aircraft to automatically land in a pre-set landing mode in response to the landing indication signal being received, detecting whether a landing control signal sent by a user is received, and, in response to the landing control signal sent by the user being received, modifying the pre-set landing mode according to the landing control signal to determine a modified landing mode. The landing control signal includes a first control signal for changing a pre-set attitude in the pre-set landing mode or a second control signal for changing a pre-set speed in the pre-set landing mode. The method further includes resuming the pre-set landing mode in response to the landing control signal being discontinued.

    Aerial vehicle powering off method and device, and aerial vehicle

    公开(公告)号:US11001387B2

    公开(公告)日:2021-05-11

    申请号:US16537281

    申请日:2019-08-09

    Abstract: A method for automatically powering off an aerial vehicle includes detecting an operating state of the aerial vehicle based on altitude information of the aerial vehicle. The attitude information includes at least one of absolute altitude information or relative altitude information. The relative altitude information includes a landing distance to a landing plane. The method further includes determining whether the operating state of the aerial vehicle indicates that the aerial vehicle has landed and, in response to a determination result that the aerial vehicle has landed, shutting down a propulsion output of the aerial vehicle.

    Polygon shaped vehicle restriction zones

    公开(公告)号:US11462116B2

    公开(公告)日:2022-10-04

    申请号:US17523847

    申请日:2021-11-10

    Abstract: Systems, methods, and devices are provided for controlling an unmanned aerial vehicle (UAV) associated with flight response measures. The flight response measure may be generated by assessing one or more flight-restriction strips, assessing at least one of a location or a movement characteristic of the UAV relative to the one or more flight-restriction strips, and directing, with aid of one or more processors, the UAV to take one or more flight response measures based on at least one of the location or movement characteristic of the UAV relative to the one or more flight-restriction strips.

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