FIELD: physics, control.
SUBSTANCE: invention relates to flight safety control systems. The method is based on including, in the on-board equipment of aircraft, a system processor which is integrated with an on-board object control system, on-board and ground-based equipment of mono-pulse secondary radar stations, operating in discrete-address mode and upgraded to mode "8", automatic dependent surveillance broadcast, Cospas-Sarsat international search and rescue system equipment installed on artificial earth navigation satellites Glonass-K1 and modifications thereof. The system processor enables to generate features of presence or absence of integrity of aircraft with subsequent transmission thereof to the crew team, control and rescue centres based on said integration, which enables to perform real-time preventive and adjustment procedures, needed to maintain the required level of flight safety from take-off to landing, as well as rapid determination of the location of the aircraft in case of emergency landing without using emergency on-board recording devices.
EFFECT: high efficiency of flight safety control systems.
2 cl, 3 dwg
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