FIELD: medical engineering. SUBSTANCE: method involves recording squeezing pressure applied by pilot to control stick and his push-pull force, variations in the path followed by control stick, pressure of pilotТs feet on pedal, position of his head, breathing process, oxygen pressure and quality of mixture in oxygen system channel, pressure within G-suit, critical altitude, present height, and G-load value. In case of deviation of recorded values from those specified, analysis and control unit generates data on abnormal situation and conveys it to pilot. As soon as pilot has eliminated it, analysis unit cancels the command sent to acoustic synthesizer; if pilot has not responded to information, unit sends signal to stimulation system for turning it on, changing the aircraft over to level flight and for turning on automatic flight and landing control systems. Device implementing this method has series-connected meter unit, analysis and control unit, and output unit. Meter unit is, essentially, set of transducers enabling all necessary measurements concerning parameters of state and those of some pieces of aircraft equipment ensuring execution of mentioned functions. EFFECT: improved confidence of the analyses of pilotТs condition and provision for rendering him immediate help. 2 cl, 1 dwg
