FIELD: radio engineering, communication.
SUBSTANCE: device for including an attitude control unit in a flight navigation system, comprising a primary information sensor unit, connected through an analogue-to-digital converter (ADC) to a computer, which is connected to a converter for converting analogue signals which are proportional to the sine and cosine of the current angle, the device further includes a heating element and a temperature sensor installed in the primary information sensor unit, and a microcontroller with a built-in ADC. An amplifier is connected between the output of the microcontroller and the heating element, and the temperature sensor is connected to the input of the ADC which is built into the microcontroller, the output of which is connected to the computer.
EFFECT: high accuracy.
1 dwg
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