FIELD: gyroscopic instrumentation.
SUBSTANCE: invention relates to a measuring technique for gyroscopic instrumentation. The essence of the invention lies in the fact that a switch of adjustment circuits of gyroscopic orientation devices in a turn has two gyroscopic angular velocity sensors connected to the first and second inputs of the parallel port of the microcontroller, which determines the angular turning velocity according to the formula:
where ti is discrete time; ωa(ti), ωz(ti) are angular velocities measured by gyroscopic angular velocity sensors.
EFFECT: invention increases efficiency of the switch for adjusting gyroscopic orientation devices when an airplane is performing a turn.
1 cl, 2 dwg
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