FIELD: instrumentation.
SUBSTANCE: invention is used in backup systems of flight navigation devices. Essence of the claimed technical solution consists in the fact that in the system, comprising a total pressure sensor, a static pressure sensor, a signal processing and conversion device, a computer, a spatial orientation module, an LCD indicator, a magnetic probe, additionally introduced is a unit for generating a feature of uniform horizontal flight, which is configured to determine threshold conditions based on readings of the magnetic field of the Earth, a switching unit, a buffer stage, an interface module.
EFFECT: higher accuracy and reliability of measuring the orientation parameters of aircraft equipment.
1 cl, 1 dwg
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