METHOD OF DISTRIBUTION OF FUNCTIONS OF AIRCRAFT CONTROL AND SYSTEM FOR ITS IMPLEMENTATION Russian patent published in 2017 - IPC G05B13/00 G06F17/40 

FIELD: aircraft engineering.

SUBSTANCE: invention relates to flight operation of aircraft (AC) and can be used in development of automated control systems. Method of allocating control functions of AC consists in fact that initial data is generated, signals on state of onboard systems are received, received signals are compared with allowable values. In case of mismatch critical system is detected, for which with due allowance for service time of blocks current probability of faultless operation and failure probability are calculated. From found values taking into account specificity of functional circuit of critical system probability of positive and negative results of system units checks is calculated. According to standard working control procedures and control of critical system pilot actions are analyzed. By results of performed operations information value of system and intensity of pilot’s actions are calculated, IQ and its limit value are determined for pilot. Signal is generated, equal to degree of situational awareness of pilot, and decision on control individual is made on basis results of comparison with limit value. Unit for evaluating degree of situational awareness of pilot on basis of onboard intelligent control system of AC configured according to algorithm is also disclosed.

EFFECT: as a result due to duplication of AC control and monitoring processes between pilot and control system (autopilot) flight safety is increased.

14 cl, 14 dwg