FIELD: measurement.
SUBSTANCE: invention relates to measurement and indication systems, which provide for piloting of aircraft in case of failure of main flight-navigation systems. Integrated system of backup devices includes a full pressure sensor, a static pressure sensor, a signal processing and conversion device, a computer, a spatial orientation module, a liquid crystal display, braking sensor, operating mode control device, car transceiver, photosensor, device for compensation of systematic component zero displacement of inertial sensors of spatial orientation module, measuring resistor, built-in control system, current stabilizer, commutator, ADC, reference voltage source, braking device control device.
EFFECT: higher safety of piloting of aircraft and reliability of system.
1 cl, 1 dwg
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