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    Aircraft control apparatus, control system and control method
    97.
    发明授权
    Aircraft control apparatus, control system and control method 有权

    公开(公告)号：US11801938B2

    公开(公告)日：2023-10-31

    申请号：US17585886

    申请日：2022-01-27

    Applicant: SZ DJI Technology Co., LTD

    Inventor： Tao Wang ,  Tao Zhao

    IPC: B64C39/02 ,  B64C13/20 ,  A63H30/04 ,  B64D47/08 ,  G05D1/00 ,  A63H27/00 ,  B64U101/30

    CPC classification number: B64C39/024 ,  A63H27/02 ,  A63H30/04 ,  B64C13/20 ,  B64D47/08 ,  G05D1/0033 ,  B64U2101/30 ,  B64U2201/20

    Abstract: An aircraft control system and control method are disclosed. The system comprises a remote control apparatus with a first control rod and a flight controller associated with an aircraft. The first control rod is configured to move in a first movement direction to control a motion of the aircraft in a first motion direction when an external force is applied on the first control rod and after a withdrawal of the external force, the first control rod returns to a preset position. The remote control apparatus operates to generate one or more control signals corresponding to the withdrawal of the external force. The flight controller controls the aircraft to maintain a flight state based on said control signals and one or more state signals, which are generated based on a measurement of the flight state by a flight controller associated with the aircraft state measurement sensors carried by the aircraft.

    Payload mounting platform
    99.
    发明授权
    Payload mounting platform 有权

    公开(公告)号：US11001395B2

    公开(公告)日：2021-05-11

    申请号：US16783586

    申请日：2020-02-06

    Applicant: SZ DJI TECHNOLOGY CO., LTD.

    Inventor： Tao Zhao ,  Xi Feng Zhao ,  Yong Wang ,  Li Zhou ,  Tao Wang

    IPC: B64D47/08 ,  F16M11/10 ,  F16M11/20 ,  F16M11/42 ,  G03B15/00 ,  F16M11/18 ,  G03B17/56 ,  B64C39/02

    Abstract: An apparatus for supporting a payload includes a payload mount configured to be coupled to the payload to secure the payload, a first support member coupled to one side of the payload mount in a single arm configuration and including a first actuation unit configured to rotate the payload mount around a first rotational axis relative to the first support member, and a single flexible member including a branched configuration. The branched configuration includes at least a first end that is electrically coupled to the payload mount and a second end that is electrically coupled to the first actuation unit.

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