FIELD: aircraft engineering.
SUBSTANCE: extra interfaces between magnetometers are arranged in every device of three-component rigidly secured magnetometer. Besides, it incorporates extra means for more precise setting of standby orientation system with due allowance for measurements of the Earth magnetic field components error in every said magnetometer of every device over one and the same period of time.
EFFECT: higher accuracy of angular velocity transducer intrinsic drift and aircraft spatial position parameters calculation.
2 cl, 2 dwg
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