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

机译:无人机包括用于补偿惯性单元温度偏差的先进装置

摘要

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.
机译:无人机的惯性单元IMU安装在主电路板上。 IMU( 26 )包括一个内部温度传感器,用于传送芯片温度信号(θ° chip )。加热组件( 36 )安装在靠近IMU的电路板上,并提供了集成到电路板上的热导,该热导在加热组件和IMU之间延伸。加热组件产生的热量传递到IMU。该热导特别地可以是结合到板上的金属平面层,特别是接地平面。温度调节电路( 44 - 62 )接收芯片温度信号(θ chip )和设定点温度信号( θ° ref ),并传送加热组件的引导信号( TH _ PWM ),从而控制向IMU。特别地,可以使用这种快速的温度升高在几分钟内完成IMU的完全校准。

著录项

  • 公开/公告号US10191080B2

    专利类型

  • 公开/公告日2019-01-29

    原文格式PDF

  • 申请/专利权人 PARROT DRONES;

    申请/专利号US201615176094

  • 申请日2016-06-07

  • 分类号G01P21;G01C19;G05D23/19;B64C39/02;G01C21/16;

  • 国家 US

  • 入库时间 2022-08-21 12:10:22

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