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    Aircraft control apparatus, control system and control method
    101.
    发明授权
    Aircraft control apparatus, control system and control method 有权

    公开(公告)号：US10717525B2

    公开(公告)日：2020-07-21

    申请号：US15465457

    申请日：2017-03-21

    Applicant: SZ DJI Technology Co., LTD

    Inventor： Tao Wang ,  Tao Zhao

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

    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
    103.
    发明授权
    Payload mounting platform 有权

    公开(公告)号：US10556708B2

    公开(公告)日：2020-02-11

    申请号：US16247066

    申请日：2019-01-14

    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 first support member coupled to the payload and a flexible member configured to be electrically coupled to the first support member and the payload. The payload is configured to rotate around a first rotational axis relative to the first support member. The flexible member is configured to (i) wind around a portion of the first support member or the payload when the payload is rotated in a first direction around the first rotational axis, and (ii) unwind from around the portion when the first support member is rotated in a second direction opposite the first direction around the first rotational axis. The flexible member is configured to transmit sensor data indicating a spatial disposition of the payload or the first support member.

    Battery and unmanned aerial vehicle with the battery
    104.
    发明授权
    Battery and unmanned aerial vehicle with the battery 有权

    公开(公告)号：US10525832B2

    公开(公告)日：2020-01-07

    申请号：US16044349

    申请日：2018-07-24

    Applicant: SZ DJI TECHNOLOGY CO., LTD.

    Inventor： Tao Zhao

    IPC: H02J7/00 ,  B60L11/18 ,  B64C39/02

    Abstract: The disclosure provides a battery which can include a power supply and power supply circuit, the power supply circuit connected to the power supply. The power supply can discharge through the power supply circuit. An electronic switch can control the power-on or off of the power supply, thereby avoiding the generation of sparks during the power on process and allowing for the normal use of the battery and the safety of the aircraft. The disclosure also provides an aircraft having the battery.

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