Drone including advance means for compensating the bias of the inertial unit as a function of the temperature

    公开(公告)号:US10191080B2

    公开(公告)日:2019-01-29

    申请号:US15176094

    申请日:2016-06-07

    Applicant: PARROT DRONES

    Abstract: The inertial unit, IMU, of the drone is mounted on a main circuit board. The IMU (26) includes an internal temperature sensor delivering a chip temperature signal (θ°chip). A heating component (36) is mounted on the circuit board near the IMU, and it is provided a thermal guide, incorporated to the circuit board, extending between the heating component and the IMU so as to allow a transfer to the IMU of the heat produced by the heating component. This thermal guide may in particular be a metal planar layer incorporated to the board, in particular a ground plane. A thermal regulation circuit (44-62) receives as an input the chip temperature signal (θchip) and a set-point temperature signal (θ°ref), and delivers a piloting signal (TH_PWM) of the heating component, so as to control the heat supply to the IMU. It is in particular possible to use this fast increase in temperature to perform a complete calibration of the IMU in a few minutes.

    DRONE INCLUDING ADVANCED MEANS FOR COMPENSATING THE BIAS OF THE INERTIAL UNIT AS A FUNCTION OF THE TEMPERATURE
    2.
    发明申请
    DRONE INCLUDING ADVANCED MEANS FOR COMPENSATING THE BIAS OF THE INERTIAL UNIT AS A FUNCTION OF THE TEMPERATURE 审中-公开
    包括用于补偿作为温度函数的惯性单位的偏差的先进手段

    公开(公告)号:US20160370404A1

    公开(公告)日:2016-12-22

    申请号:US15176094

    申请日:2016-06-07

    Applicant: PARROT DRONES

    CPC classification number: G01P21/00 B64C39/024 G01C19/00 G01C21/16 G05D23/1919

    Abstract: The inertial unit, IMU, of the drone is mounted on a main circuit board. The IMU (26) includes an internal temperature sensor delivering a chip temperature signal (θ°chip). A heating component (36) is mounted on the circuit board near the IMU, and it is provided a thermal guide, incorporated to the circuit board, extending between the heating component and the IMU so as to allow a transfer to the IMU of the heat produced by the heating component. This thermal guide may in particular be a metal planar layer incorporated to the board, in particular a ground plane. A thermal regulation circuit (44-62) receives as an input the chip temperature signal (θchip) and a set-point temperature signal (θ°ref), and delivers a piloting signal (TH_PWM) of the heating component, so as to control the heat supply to the IMU. It is in particular possible to use this fast increase in temperature to perform a complete calibration of the IMU in a few minutes.

    Abstract translation: 无人机的惯性单元IMU安装在主电路板上。 IMU(26)包括提供芯片温度信号(θ°芯片)的内部温度传感器。 加热部件(36)安装在靠近IMU的电路板上,并且设置有一个热引导件,该引导件结合到电路板上,在加热部件和IMU之间延伸,以便允许传送到IMU的热量 由加热部件产生。 该导热器可以特别地是与基板结合的金属平面层,特别是接地平面。 热调节电路(44-62)接收芯片温度信号(θchip)和设定点温度信号(θ°ref)作为输入,并传送加热部件的导频信号(TH_PWM),以便控制 向IMU供热。 特别是可以在几分钟内使用这种快速增加的温度来完成IMU的完整校准。

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