FIELD: instrument making.
SUBSTANCE: system comprises a primary detection circuit, which includes at least one measurement channel. At the same time the specified measurement channel comprises the following: a device to measure static air pressure; a device to measure sideslip angle of an aircraft; a device to measure dynamic pressure, common temperature and angle of aircraft attack; a device of data processing made as capable of detecting anemobaroclinometric parameters on the basis of measurements of static pressure, sideslip angle, dynamic pressure, common temperature and attack angle; at least one laser anemometer (50) to measure at least one parameter of actual speed of the aircraft.
EFFECT: reliability improvement.
6 cl, 4 dwg
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