FIELD: measuring systems.
SUBSTANCE: invention relates to systems for measurement and indication, and can be applied to systems, which provide pilotage of aircraft (AC) in case of failure of main pilotage and navigation systems. For this purpose, device for entering and selection of deviation coefficients is additionally introduced into integrated system of backup devices. At that, magnetic field sensor calibration is executed, wherefrom deviation coefficients are determined for perturbed of magnetic field independent useful load objects.
EFFECT: technical result is increase of accuracy.
2 cl, 1 dwg
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