FIELD: aviation; measurement technology.
SUBSTANCE: invention relates to measurement and indication systems, which provide for piloting of aircraft in case of failure of main flight-navigation systems. Invention is an integrated backup device system comprising full and static pressure sensors, signal processing and conversion device, computer, a spatial orientation module, a mode control device, a magnetic probe, a liquid crystal display, a slip indicator, a photosensor, device for compensation of systematic component of zero shift of inertial sensors of spatial orientation module, deviation error recording device with memory, built-in monitoring system, device for interface exchange, connected by input to calculator, and by output—to introduced galvanic decoupling device.
EFFECT: technical result is higher reliability of aircraft and flight safety.
1 cl, 1 dwg
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