This invention belongs to the field of navigation instrument technology and discloses an inertial navigation instrument with automatic
temperature control function, including a main body and a
power supply unit, and further including: a heat conduction component installed inside the main body; wherein, the heat conduction component includes a heat absorption head fixedly connected to the inside of the main body, a connecting shell fixedly installed inside the main body, and a connecting
pipe located inside the connecting shell fixedly installed on one side of the heat absorption head; this invention forms a directional
heat flow blowing towards the surface of the
gyroscope and
accelerometer, and finally utilizes the heat generated by the operation of the
power supply unit to drive a motor to squeeze the surface of the connecting
pipe, thereby guiding the heat to the surface of the
gyroscope and
accelerometer, so that the
gyroscope and
accelerometer can reach and maintain a suitable
operating temperature range, ensuring the normal operation of the gyroscope and accelerometer, and improving the overall performance of the
navigation system.